Impact of Aerodynamic and Structural Parameters on Control Surface Buzz-Reference-Cited by-同舟云学术

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Impact of Aerodynamic and Structural Parameters on Control Surface Buzz

Published:2021-12-16 Issue: Volume: Page:1-12
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Pai Fang-Ping¹^ORCID,Yang Lee-Jang¹,Huang Ying-Hsuan¹,Chen P. C.²

Affiliation:

1. National Chung Shan Institute of Science and Technology, Taichung 407, Taiwan

2. ZONA Technology, Inc., Scottsdale, Arizona 85258

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060675

Reference18 articles.

1. SaitoH. “On the Aileron Buzz in Transonic Flow,” Univ. of Tokyo Aeronautical Research Inst. Rept. 346, Tokyo, Japan, July 1959.

2. LambourneN. C. “Control Surface Buzz,” Aircraft Research Council R&M 3364, Her Majesty’s Stationery Office, London, 1964.

3. EricksonA. L.StephensonJ. D. “A Suggestion Method of Analyzing for Transonic Flutter of Control Surfaces Based on Available Experimental Evidence,” NACA RM A7F30, Dec. 1947.

4. NakamuraY.TanabeY. “Some Experiments on Control-Surface Buzz,” National Aerospace Lab. TR-72T, Chofu, Tokyo, Japan, Nov. 1964.

5. Experimental Investigation of Hypersonic Buzz on a Delta Configuration

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